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Redshift Between Emission and Reception

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A redshift compares two local frequency measurements linked by one propagating light signal. The emitter and receiver contribute their four-velocities at different events, while the null wave vector carries the phase information between them. The exact ratio is coordinate independent, but splitting it into “Doppler” and “gravitational” pieces requires an additional reference frame or spacetime symmetry.

Required background. Observers, Rest Spaces, and Measured Components provides observer projectors and measured decompositions; Pseudo-Riemannian Metrics and Signature provides Lorentzian norms and causal classification; Frames, Coframes, and Anholonomy provides dual frames and local Lorentz freedom.

Helpful background. Events, Intervals, and Minkowski Geometry supplies the flat-spacetime limit; Tensor Fields and Natural Operations clarifies tensors versus their components; Killing Fields and Isometry Groups supplies the stationary conserved quantity; The Wave Equation and Characteristics connects the geometric-optics phase to its transported wave vector.

Let a geometric-optics light ray connect emission event ee to reception event rr. Its future-directed null wave vector is kμk^\mu, with the same phase normalization transported along the ray. If the emitter and receiver have four-velocities ueμu_e^\mu and urμu_r^\mu, each measures

ωe=−(kμueμ)e,ωr=−(kμurμ)r.\omega_e=-(k_\mu u_e^\mu)_e, \qquad \omega_r=-(k_\mu u_r^\mu)_r.

Define the redshift by 1+z=λr/λe=ωe/ωr1+z=\lambda_r/\lambda_e=\omega_e/\omega_r. Therefore

1+z=(−k⋅u)e(−k⋅u)r.1+z =\frac{(-k\cdot u)_e}{(-k\cdot u)_r}.

The signs are essential with u2=−1u^2=-1: both contractions are positive for a future-directed wave and future-directed observer. A positive zz means the received frequency is smaller. An overall constant rescaling of kμk^\mu cancels between endpoints, although a physical wave train fixes its normalization through the phase.

The ratio also has a direct clock interpretation. Follow two neighboring wave crests from the emitter to the receiver along the same smoothly varying ray branch. The number of phase cycles is unchanged during propagation, so the magnitudes of the phase increments satisfy

ωe dτe=ωr dτr,1+z=dτrdτe.\omega_e\,d\tau_e=\omega_r\,d\tau_r, \qquad 1+z=\frac{d\tau_r}{d\tau_e}.

A redshift therefore means a longer received interval between successive crests. This is a differential comparison of nearby pulses; a long evolving pulse train need not have one constant redshift.

The formula assumes geometric optics and a specified null path. If lensing produces several rays between the same worldlines, each image can have a different kμk^\mu and hence a different redshift and arrival time. If there is no connecting ray, no such comparison exists.

There is no invariant, observer-free relative velocity between separated events. To organize the result, choose a smooth reference observer field nμn^\mu at the two endpoints. Multiplying by unity gives the exact factorization

1+z=(−k⋅ue)e(−k⋅n)e(−k⋅n)e(−k⋅n)r(−k⋅n)r(−k⋅ur)r.1+z =\frac{(-k\cdot u_e)_e}{(-k\cdot n)_e} \frac{(-k\cdot n)_e}{(-k\cdot n)_r} \frac{(-k\cdot n)_r}{(-k\cdot u_r)_r}.

The first and third factors are local Doppler comparisons between the physical endpoint observers and nμn^\mu. The middle factor is the frequency change measured by the chosen reference congruence along propagation. A different nμn^\mu redistributes the factors while leaving their product fixed. Thus the total redshift is observable, but a generic motion-versus-geometry split is not unique.

In flat spacetime, take an inertial reference field and a photon moving in the +x+x direction. A receiver receding at speed vv measures ωr=γ(1−v)ωe\omega_r=\gamma(1-v)\omega_e, so

1+z=1+v1−v.1+z=\sqrt{\frac{1+v}{1-v}}.

This special-relativistic limit checks the endpoint signs: recession gives z>0z>0, approach gives z<0z<0.

Suppose the relevant region admits a timelike Killing field ξμ\xi^\mu. Along an affinely parametrized null geodesic,

E=−ξμkμ\mathcal E=-\xi_\mu k^\mu

is constant, because kν∇ν(ξμkμ)=kμkν∇(μξν)=0k^\nu\nabla_\nu(\xi_\mu k^\mu)=k^\mu k^\nu\nabla_{(\mu}\xi_{\nu)}=0. Observers following the Killing flow have

uμ=ξμN,N=−ξμξμ,u^\mu=\frac{\xi^\mu}{N}, \qquad N=\sqrt{-\xi^\mu\xi_\mu},

so they measure ω=E/N\omega=\mathcal E/N. For a stationary emitter and receiver connected by the ray,

1+z=NrNe.1+z=\frac{N_r}{N_e}.

The normalization of ξμ\xi^\mu cancels from this ratio. The formula applies only where the chosen Killing field is timelike and the observers actually follow its integral curves. It is not a general formula for dynamical spacetimes, rotating observers not aligned with ξμ\xi^\mu, or arbitrary moving endpoints.

In a weak, static field with g00=−(1+2Φ)+O(Φ2)g_{00}=-(1+2\Phi)+O(\Phi^2), N=1+Φ+O(Φ2)N=1+\Phi+O(\Phi^2) and

z=Φr−Φe+O(Φ2).z=\Phi_r-\Phi_e+O(\Phi^2).

A signal climbing to larger Newtonian potential is redshifted. The equivalence-principle derivation and curved-clock interpretation are given in Reall 2013, Ch. 1, pp. 6–10, PDF and Carroll 1997, Ch. 4, pp. 101–104.

Redshift compares clock rates only after a light-transfer protocol and source frequency standard are specified. It is not an intrinsic property located “inside the photon,” nor does it define a global distance. Absorption, dispersion, plasma propagation, finite wave packets, source evolution, detector response, and failure of geometric optics can alter what a real spectrometer infers; those effects lie beyond the vacuum null-ray model used here.

Even in vacuum, a conserved coordinate component such as ktk_t has physical meaning only when tied to a symmetry and its normalization. The endpoint contractions remain the general statement. They cleanly separate what is measured locally from what must be propagated through the spacetime between measurements.

In a static region, two observers follow the same timelike Killing field at lapse values NeN_e and Nr=2NeN_r=2N_e. A monochromatic signal is emitted by the first and received by the second. Find the frequency ratio and redshift.

Solution

The conserved Killing energy gives ωe=E/Ne\omega_e=\mathcal E/N_e and ωr=E/Nr=ωe/2\omega_r=\mathcal E/N_r=\omega_e/2. Hence

1+z=ωeωr=2,z=1.1+z=\frac{\omega_e}{\omega_r}=2, \qquad z=1.

The receiver measures half the emitted frequency. The result assumes both observers are stationary with respect to the same Killing flow and that the connecting null ray stays within the stationary region.